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Simplified Two‐Dimensional Aerofoil Theory: A Basic Method of Determining the Profiles of Laminar Flow and High‐Speed Aerofoils

M.J. Brennan B.Sc., A.F.R.Ae.S. (Saunders‐Roe Ltd., I.O.W.)
A.C. Stevenson M.Sc. (University College, London)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 June 1946

64

Abstract

THIS article derives from one of similar title by H. J. Stewart, in which he gave an account of a simple method of dealing with thin aerofoil theory for small angles of incidence by satisfying the usual approximate condition at the boundary of the aerofoil after expanding the slope of the profile in a Fourier series.

Citation

Brennan, M.J. and Stevenson, A.C. (1946), "Simplified Two‐Dimensional Aerofoil Theory: A Basic Method of Determining the Profiles of Laminar Flow and High‐Speed Aerofoils", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 6, pp. 182-194. https://doi.org/10.1108/eb031377

Publisher

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MCB UP Ltd

Copyright © 1946, MCB UP Limited

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